Abstract: A rotary wing aircraft includes a main rotor; an electric motor for rotating the main rotor; an electric generator for supplying electric power to the electric motor; an engine for driving the generator; and battery storage for providing battery power. The aircraft further includes a flight control system for controlling the engine to run at idle and causing the electric motor to receive the battery power to rotate the main rotor during takeoff; for controlling the engine to increase speed above idle and operate the generator to recharge the battery storage during flight; and for controlling the engine to return to idle and controlling the electric motor to receive the battery power for landing.

Abstract: A rotary wing aircraft includes a main rotor; an electric motor for rotating the main rotor; an electric generator for supplying electric power to the electric motor; an engine for driving the generator; and battery storage for providing battery power. The aircraft further includes a flight control system for controlling the engine to run at idle and causing the electric motor to receive the battery power to rotate the main rotor during takeoff; for controlling the engine to increase speed above idle and operate the generator to recharge the battery storage during flight; and for controlling the engine to return to idle and controlling the electric motor to receive the battery power for landing.

Abstract: A helicopter has a propulsion system that includes a diesel engine driven electric generator, battery storage, power inverters for converting AC current to DC current and converting DC current to AC current, and an electric motor powered main rotor and an electric motor powered tail rotor. The propulsion system is integrated with electric controls of the main rotor electric motor and the tail rotor electric motor to provide additional system efficiencies. The design of the helicopter allows a single engine helicopter to be just as safe as a twin engine design helicopter while consuming less fuel. The helicopter design also includes a main rotor tilt system which tilts the rotation axis of the main rotor forward during high-speed flight to improve the aerodynamic efficiency of the helicopter airframe and rotary wing.

Abstract: The present disclosure provides a method for navigation of a vehicle using cellular networks that involves determining, with an inertial navigation system, a vehicle location estimate. The method also involves transmitting, with a transmit antenna, a transmit signal to the cellular tower requesting a cell identification (CID); and receiving, with a receive antenna, a receive signal from the cellular tower containing the CID. Further, the method involves determining the cellular tower location by looking up the CID in a lookup table; determining a difference in time from the time the transmit signal was sent to the time the receive signal was received; calculating the distance from the vehicle to the cellular tower by using the time difference; and refining the vehicle location estimate by using the cellular tower location, the distance from the vehicle to the cellular tower, and the angle of the transmit antenna and the receive antenna.

Abstract: The present disclosure provides a method for navigation of a vehicle using cellular networks that involves determining, with an inertial navigation system, a vehicle location estimate. The method also involves transmitting, with a transmit antenna, a transmit signal to the cellular tower requesting a cell identification (CID); and receiving, with a receive antenna, a receive signal from the cellular tower containing the CID. Further, the method involves determining the cellular tower location by looking up the CID in a lookup table; determining a difference in time from the time the transmit signal was sent to the time the receive signal was received; calculating the distance from the vehicle to the cellular tower by using the time difference; and refining the vehicle location estimate by using the cellular tower location, the distance from the vehicle to the cellular tower, and the angle of the transmit antenna and the receive antenna.